[1]
Xiaohua Gan, Aero gas gurbine engine fuel nozzle technology[M]. Beijing, 2006: 22-23. (in Chinese).
Google Scholar
[2]
Schweitzer P H. Mechanism of disintegration of liquid jets [J]. Journal of Applied Physics, 1937, 8(8): 513-521.
Google Scholar
[3]
Abramovich G N, Girshovich T A, Krasheninnikov S I, et al. The theory of turbulent jets [J]. Moscow Izdatel Nauka, 1984, 1.
Google Scholar
[4]
K. Yokota, S. Matsuoka. An experimental Study of Fuel Spray in a Diesel Engine [J]. JSME, 1977, Vol. 43: 373~383.
Google Scholar
[5]
Reitz R D, Bracco F B. On the dependence of spray angle and other spray parameters on nozzle design and operating conditions [J]. Future, 1979, 2012: 12-11.
DOI: 10.4271/790494
Google Scholar
[6]
F. Ruiz and N. Chigier, The Mechanics of High Speed Atomization, Proc. 3rd Int. Conf. Liquid Atomization and Spray Systems, London, pp. VIB/3/l-15, (1985).
Google Scholar
[7]
Guixiang Yang,Rushan Jin. Characteristics of the Liquid Fuel Atomization in Heated Air Flow [J] Journal of Aerospace Power. 1989, 1(1): 76-78. (in Chinese).
Google Scholar
[8]
Inamura T, Takahashi M, Kumakawa A. Combustion characteristics of a liquid-fueled ramjet combustor[J]. Journal of Propulsion and Power, 2001, 17(4): 860-868.
DOI: 10.2514/2.5817
Google Scholar
[9]
Kris B, Jong L, Domenic S. Characterization of Liquid Jets-In-Crossflow Under High Temperature, High Velocity Non-Oscillating and Oscillating Flow Conditions; proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006 [C]. American Institute of Aeronautics and Astronautics.
DOI: 10.2514/6.2006-1225
Google Scholar
[10]
Johnson J N, Lubarsky E, Zinn B T. Experimental Investigation of Spray Dynamics Under Jet Engine Augmentor Conditions[C]. AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 2005: 1-15.
DOI: 10.2514/6.2005-4480
Google Scholar
[11]
Chin J S,Lefebvre A H.Semi-Empirical Analysis of Liquid Fuel and Fuel Vapor Distribution Downstream of a Plain-Orifice Injector with Cross-Stream Air Flow[R].AIAA 85-1320.
DOI: 10.2514/6.1985-1320
Google Scholar
[12]
Yang Liu, Jie Jin, Yuying Liu, et al. Experiment of drag characteristics of a novel variable geometry flame-holder[J]. Journal of Aerospace Power. 2011, 26(11): 2485-2494.
Google Scholar
[13]
Hiroyasu H. Diesel engine combustion and its modeling[C]. Proceedings of 1st International Symposium on Diagnostics and Modeling of Combustion in internal Combustion Engines. Tokyo, Japan. 1985: 53-75.
DOI: 10.1299/jmsesdm.2004.6.167
Google Scholar
[14]
Shengyong Li; Mouwei Li; Shaojun Zhang; Bangwen Wang. Study on the Breakup Length of Circular Impinging Jet[J]. Journal of University of Science and Technology Beijing, 2007, 14(6): 585-588.
DOI: 10.1016/s1005-8850(07)60133-9
Google Scholar
[15]
Sallam K A, Dai Z, Faeth G M. Liquid Breakup at the Surface of Turbulent Round Liquid Jets in Still Gases[J]. International Journal of Multiphase Flow, 2002, 28(3): 427-449.
DOI: 10.1016/s0301-9322(01)00067-2
Google Scholar
[16]
Lingyun Hou, Xiaochun Hou. Nozzle Technical Manual [M]. Beijing, 2002 : 78. (in Chinese).
Google Scholar
[17]
Ding H, Huang D, et al. Experiment study on spray structure of a multi-hole GDI injector[C]. Electric Information and Control Engineering (ICEICE), 2011 International Conference on. IEEE, 2011: 5901-5904.
DOI: 10.1109/iceice.2011.5777127
Google Scholar